Patent classifications
C22C1/02
METHOD FOR FLEXIBLE MANUFACTURING OF INTERMETALLIC COMPOUNDS AND DEVICE FOR MAKING THEREOF
The invention relates to a method and apparatus for the flexible manufacture of intermetallic compounds, including those with shape memory effect. The method and the device can find mass application in the industrial production of modern functional and innovative products based on intermetallic compounds with predetermined physicomechanical parameters and properties. The method includes the steps of taking an intermediate sample of the meld, measuring the actual physico-mechanical properties and material characteristics of the sample and tuning the composition and/or the operating mode parameters of the melting furnace. The device includes measuring module (I) and module (II) for displaying and storing information.
IMPLANT MAGNESIUM ALLOY, BONE FIXTURE, METHOD OF MANUFACTURING IMPLANT MAGNESIUM ALLOY, AND METHOD OF MANUFACTURING BONE FIXTURE DEVICE
Provided is an implant magnesium alloy having corrosion resistance, mechanical strength, ductility at the same time. In one aspect of the present invention, an implant magnesium alloy contains: x at % of Zn; a total of y at % of at least one element of Ca and Sr; and the balance of Mg and inevitable impurities. x and y satisfy formulae 1 and 2:
0.15≤x≤1.5 (Formula 1)
0.5≤y≤1.5. (Formula 2)
IMPLANT MAGNESIUM ALLOY, BONE FIXTURE, METHOD OF MANUFACTURING IMPLANT MAGNESIUM ALLOY, AND METHOD OF MANUFACTURING BONE FIXTURE DEVICE
Provided is an implant magnesium alloy having corrosion resistance, mechanical strength, ductility at the same time. In one aspect of the present invention, an implant magnesium alloy contains: x at % of Zn; a total of y at % of at least one element of Ca and Sr; and the balance of Mg and inevitable impurities. x and y satisfy formulae 1 and 2:
0.15≤x≤1.5 (Formula 1)
0.5≤y≤1.5. (Formula 2)
MULTICOMPONENT FECOSIM SOFT MAGNETIC ALLOY AND PREPARATION METHOD THEREOF
A multicomponent FeCoSiM soft magnetic alloy is provided. M of the alloy is one or more of V, Cr and Ni. A sum of atomic percentages of alloy elements in the alloy is 100%. The atomic percents of the alloy elements meet the following conditions: Fe, 68˜78 at %; Co, 4˜12 at %; Si, 14˜18 at %; V, 0˜4 at %; Cr, 0˜4 at %; and Ni, 0˜4 at %. The preparation method of the alloy includes weighing raw materials according to the atomic percentages of the alloy elements and then performing melting and annealing heat treatment each in vacuum or a protective atmosphere. The alloy is obtained by a reasonable design of compositions and contents. A magnetocrystalline anisotropy constant of the alloy is low, a magnetostrictive coefficient of the alloy approaches zero and the alloy has characteristics of high saturation flux density and low coercivity.
EQUIPMENT AND METHOD FOR MANUFACTURING COPPER ALLOY MATERIAL
A copper alloy material manufacturing equipment for manufacturing a copper alloy material by continuously casting molten copper. The equipment includes an element adding means for adding a metal element to the molten copper, a tundish for holding the molten copper containing the metal element, a pouring nozzle connected to the tundish to feed the molten copper from the tundish, and a trapping member arranged inside the tundish and including a same type of material as at least one of an oxide of the metal element, a nitride of the metal element, a carbide of the metal element and a sulfide of the metal element.
EQUIPMENT AND METHOD FOR MANUFACTURING COPPER ALLOY MATERIAL
A copper alloy material manufacturing equipment for manufacturing a copper alloy material by continuously casting molten copper. The equipment includes an element adding means for adding a metal element to the molten copper, a tundish for holding the molten copper containing the metal element, a pouring nozzle connected to the tundish to feed the molten copper from the tundish, and a trapping member arranged inside the tundish and including a same type of material as at least one of an oxide of the metal element, a nitride of the metal element, a carbide of the metal element and a sulfide of the metal element.
(Zr,Hf)3Ni3Sb4-based n-type thermoelectric conversion material
An n-type thermoelectric conversion material expressed in a chemical formula X.sub.3-xX′.sub.xT.sub.3-yCu.sub.ySb.sub.4 (0≦x<3, 0≦y<3.0, and x+y>0), the X includes one or more element(s) of Zr and Hf, the X′ includes one or more element(s) of Nb and Ta, and the T includes one or more element(s) selected from Ni, Pd, and Pt, while including at least Ni, the n-type thermoelectric conversion material expressed in the chemical formula X.sub.3-xX′.sub.xT.sub.3-yCu.sub.ySb.sub.4 has symmetry of a cubic crystal belonging to a space group I-43d.
(Zr,Hf)3Ni3Sb4-based n-type thermoelectric conversion material
An n-type thermoelectric conversion material expressed in a chemical formula X.sub.3-xX′.sub.xT.sub.3-yCu.sub.ySb.sub.4 (0≦x<3, 0≦y<3.0, and x+y>0), the X includes one or more element(s) of Zr and Hf, the X′ includes one or more element(s) of Nb and Ta, and the T includes one or more element(s) selected from Ni, Pd, and Pt, while including at least Ni, the n-type thermoelectric conversion material expressed in the chemical formula X.sub.3-xX′.sub.xT.sub.3-yCu.sub.ySb.sub.4 has symmetry of a cubic crystal belonging to a space group I-43d.
Methods for producing 2024 and 7075 aluminum alloys by recycling waste aircraft aluminum alloys
The present invention relates to techniques for producing 2024 and 7075 aluminum alloys by recycling waste aircraft aluminum alloys, which belong to technical fields for circular economy. The present invention develops techniques for obtaining the 2024 and 7075 aluminum alloys by subjecting waste aircraft aluminum alloys as raw materials to pretreatment, smelting, impurity removal, melt ingredient assay, ingredient adjustment, refining, and casting. Through utilizing the waste package aluminum alloys and the waste aluminum pop-top cans to adjust the ingredients, the waste aircraft aluminum alloys would be recycled at a lower cost without downgrading. The present invention has some advantages, such as low cost, and applicability for industrial production, as well as prominent economic benefit.
Methods for producing 2024 and 7075 aluminum alloys by recycling waste aircraft aluminum alloys
The present invention relates to techniques for producing 2024 and 7075 aluminum alloys by recycling waste aircraft aluminum alloys, which belong to technical fields for circular economy. The present invention develops techniques for obtaining the 2024 and 7075 aluminum alloys by subjecting waste aircraft aluminum alloys as raw materials to pretreatment, smelting, impurity removal, melt ingredient assay, ingredient adjustment, refining, and casting. Through utilizing the waste package aluminum alloys and the waste aluminum pop-top cans to adjust the ingredients, the waste aircraft aluminum alloys would be recycled at a lower cost without downgrading. The present invention has some advantages, such as low cost, and applicability for industrial production, as well as prominent economic benefit.